AROW++ // ARTEMIS II ORION TELEMETRY

ARTEMIS REAL-TIME ORBIT WEBSITE — EXTENDED

◉ CONNECTING... LAST UPDATE: — NEXT REFRESH: —

◈ NAVIGATION // DISTANCE

— KM FROM EARTH

DISTANCE TO MOON —

DECLINATION —

RIGHT ASCENSION —

ANGLE 1 —

ANGLE 2 —

ANGLE 3 —

◈ VELOCITY VECTOR // INERTIAL

— M/S TOTAL SPEED

—

ECI VELOCITY COMPONENTS (M/S)

Vx

—

Vy

—

Vz

—

ECI POSITION VECTOR (METERS)

Px

—

Py

—

Pz

—

◈ SPACECRAFT ATTITUDE // ORIENTATION

ATTITUDE QUATERNION (ECI BODY FRAME)

Q₁ (x)

—

Q₂ (y)

—

Q₃ (z)

—

Q₄ (w)

—

DERIVED EULER ANGLES (ZYX)

ROLL

—

degrees

PITCH

—

degrees

YAW

—

degrees

QUATERNION NORM —

STATUS FLAGS —

◈ MISSION STATUS

ACTIVITY —

FILE TYPE —

PHASE CODE —

PHASE NAME —

FILE TIMESTAMP —

TELEMETRY TIME —

TIME SYS UNIX EPOCH (UTC)

TOTAL PARAMS —

PARAMS OK —

◈ ANGULAR / SENSOR DATA (P2048–P2103)

VECTOR GROUP A (P2048–P2056)

P2048

—

P2049

—

P2050

—

P2051

—

P2052

—

P2053

—

P2054

—

P2055

—

P2056

—

GYRO / RATE DATA (P2096–P2098)

P2096

—

P2097

—

P2098

—

ACCEL / DELTA-V (P2101–P2103)

P2101

—

P2102

—

P2103

—

◈ TIMING // EPOCH DATA

P5010 (UTC) —

P5011 (UTC) —

P5012 (UTC) —

P5013 (UTC) —

ELAPSED (MET) —

LAUNCH DATE 2026-04-02 03:07:49 UTC

P5002–P5006 (ANGULAR / RATES)

P5002—

P5003—

P5004—

P5005—

P5006—